N2995W

Substantial
None

Bell 206BS/N: 1192

Accident Details

Date
Thursday, September 15, 2005
NTSB Number
CHI05CA271
Location
Elk Point, SD
Event ID
20051014X01651
Coordinates
42.641666, -96.686668
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of directional control for undetermined reasons which led to the pilot not being able to maintain clearance from the embankment during the forced landing. The rising embankment was a factor.

Aircraft Information

Registration
Make
BELL
Serial Number
1192
Engine Type
Turbo-shaft
Year Built
1973
Model / ICAO
206BB06
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
5
FAA Model
206B

Registered Owner (Current)

Name
SCOTTS HELICOPTER SERVICES INC
Address
PO BOX 92
City
LE SUEUR
State / Zip Code
MN 56058-0092
Country
United States

Analysis

On September 15, 2005, about 1830 central daylight time, a Bell 206B, N2995W, piloted by a commercial pilot, sustained substantial damage during a forced landing following an uncommanded right rotation near Elk Point, South Dakota. The 14 CFR Part 137 aerial application flight was operating in visual meteorological conditions without a flight plan. The pilot was not injured. The local flight was originating at the time of the accident.

According to the pilot's written statement, he had departed from the shoreline of the Mississippi river into a 2 to 3 mile per hour wind. He stated that when the helicopter was about 100 feet in altitude, 100 yards from the shore, and indicating over 50 miles per hour, a slight right turn was initiated. He stated that full left pedal input would not stop the right turn. The pilot elected to return to the shore. He stated that as he approached a flat area, he felt that he would not be able to reach the intended landing area and attempted to turn back toward the river. He said that the left rear skid contacted the sloping ground and the helicopter slid down the slope and cam to rest on its left side.

Examination of the helicopter subsequent to the accident failed to reveal any anomalies. Continuity of the tail rotor drive and control systems were confirmed. A maintenance record entry dated September 14, 2005 indicated that the tailboom had been replaced. Determination of proper rigging of the tail rotor could not be determined due to bending of the tail rotor control push-pull tubes from impact forces.

The pilot reported unlimited visibility, a temperature of 70 degrees Fahrenheit, and south winds at 2 to 3 miles per hour.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI05CA271